Damage tolerant design and analysis of current and future aircraft structure

AIAA\ICAS International Air and Space Symposium and Exposition: The Next 100 Years

Volumn , Issue , 2003, Pages

  Schmidt, Hans Jürgen ^a   Schmidt Brandecker, Bianka ^a  

^a AIRBUS OPERATIONS GMBH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE INDUSTRY; AIRFRAMES; FUSELAGES; INDUSTRIAL ENGINEERING; PRODUCTION ENGINEERING; STRUCTURAL DESIGN; TRANSPORT AIRCRAFT;

ADVANCED MATERIALS; AIRWORTHINESS REGULATIONS; ASSEMBLED STRUCTURES; DAMAGE-TOLERANT DESIGN; DIRECT OPERATING COSTS; FUSELAGE STRUCTURES; MAINTENANCE REQUIREMENT; MANUFACTURING PROCESS;

AIRCRAFT MANUFACTURE;

EID: 84896323350     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Swift, T., Fail-safe design requirements and features, regulatory requirements. Presented at the International Air & Space Symposium and Exhibition "The Next 100 Years", Dayton, USA, 2003
2. N.N., Recommendations for Regulatory Action to Prevent Widespread Fatigue Damage in the Commercial Airplane Fleet, Airworthiness Assurance Working Group - Task Planning Group, final report, revision A, June 1999
3. Homan, J., Damage Tolerance Analysis in Glare. TU Delft, Faculty of Aerospace Engineering. Presented during an internal Airbus meeting, 2002
4. Dalle Donne, C. and Raimbeaux, G., Residual stress effects on fatigue crack propagation in friction stir welds. German Aerospace Center, Institute for material Research, Cologne, Germany.